DE602006012795D1 - Vorrichtung zur Regelung der relativen Positionen von einer Gruppe in Formation fliegender Raumschiffe durch Analyse von Zweifrequenzsignalen - Google Patents

Vorrichtung zur Regelung der relativen Positionen von einer Gruppe in Formation fliegender Raumschiffe durch Analyse von Zweifrequenzsignalen

Info

Publication number
DE602006012795D1
DE602006012795D1 DE602006012795T DE602006012795T DE602006012795D1 DE 602006012795 D1 DE602006012795 D1 DE 602006012795D1 DE 602006012795 T DE602006012795 T DE 602006012795T DE 602006012795 T DE602006012795 T DE 602006012795T DE 602006012795 D1 DE602006012795 D1 DE 602006012795D1
Authority
DE
Germany
Prior art keywords
frequency signals
spaceships
flying
analyzing
formation
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
DE602006012795T
Other languages
German (de)
English (en)
Inventor
Christian Mehlen
Estelle Pierre
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Thales SA
Original Assignee
Thales SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Thales SA filed Critical Thales SA
Publication of DE602006012795D1 publication Critical patent/DE602006012795D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1085—Swarms and constellations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242—Orbits and trajectories
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/0009—Transmission of position information to remote stations
    • G01S5/0072—Transmission between mobile stations, e.g. anti-collision systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
    • G01S5/0247—Determining attitude
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
    • G01S5/0284—Relative positioning

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Astronomy & Astrophysics (AREA)
  • Automation & Control Theory (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Control Of Position Or Direction (AREA)
  • Details Of Aerials (AREA)
DE602006012795T 2006-01-19 2006-01-19 Vorrichtung zur Regelung der relativen Positionen von einer Gruppe in Formation fliegender Raumschiffe durch Analyse von Zweifrequenzsignalen Active DE602006012795D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP06300040A EP1813957B1 (fr) 2006-01-19 2006-01-19 Dispositif de contrôle de position(s) relative(s) par analyse de signaux bi-fréquences, pour un engin spatial d'un groupe d'engins spatiaux en formation

Publications (1)

Publication Number Publication Date
DE602006012795D1 true DE602006012795D1 (de) 2010-04-22

Family

ID=36579413

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006012795T Active DE602006012795D1 (de) 2006-01-19 2006-01-19 Vorrichtung zur Regelung der relativen Positionen von einer Gruppe in Formation fliegender Raumschiffe durch Analyse von Zweifrequenzsignalen

Country Status (9)

Country Link
US (1) US8463467B2 (fr)
EP (1) EP1813957B1 (fr)
JP (1) JP5007467B2 (fr)
CN (1) CN101375176B (fr)
AT (1) ATE460680T1 (fr)
DE (1) DE602006012795D1 (fr)
ES (1) ES2340062T3 (fr)
RU (1) RU2419807C2 (fr)
WO (1) WO2007082929A1 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2529185T3 (es) * 2007-04-27 2015-02-17 Alcatel Alenia Space Italia S.P.A. Determinación de la posición y de la orientación
CN103493293B (zh) * 2011-02-25 2015-08-26 霍尼韦尔国际公司 用于提供改进的tcas方位测量的系统和方法
FR2976087B1 (fr) * 2011-06-01 2019-07-12 Thales Systeme de localisation geographique d'un emetteur de signaux radioelectriques situee a la surface de la terre, et procede associe d'interferometrie distribuee
CN102981175B (zh) * 2012-12-24 2014-04-30 北京理工大学 一种集群空间机器人主从式目标协同定位方法
RU2537818C1 (ru) * 2013-07-16 2015-01-10 Открытое акционерное общество "Российская корпорация ракетно-космического приборостроения и информационных систем" (ОАО "Российские космические системы") Способ коррекции траектории полета космического аппарата и устройство для его реализации
FR3017213B1 (fr) 2014-01-31 2016-02-05 Thales Sa Procede et systeme radiofrequence de determination, par couple d'engins spatiaux, de la position angulaire relative entre plusieurs engins spatiaux distants
TWI534453B (zh) * 2014-02-18 2016-05-21 原相科技股份有限公司 相對位置定位系統與追蹤系統
CN106094862A (zh) * 2016-06-22 2016-11-09 陕西宝成航空仪表有限责任公司 无人机编队飞行通信控制的实现方法
DE102017102481A1 (de) * 2017-02-08 2018-08-09 Klaus Schilling Formationsfähiger Kleinstsatellit und Formation aus mehreren Kleinstsatelliten
CN108910086B (zh) * 2018-06-14 2024-03-15 南京邮电大学 一种基于小卫星星团的可再入式立方星系统
EP3714287B1 (fr) * 2019-02-13 2021-09-22 Lambda: 4 Entwicklungen GmbH Mesure de la durée de fonctionnement basée sur la commutation de fréquence

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3290677A (en) * 1962-12-31 1966-12-06 Trw Inc Continuous wave angle and range determining radar
JP2660017B2 (ja) * 1988-10-05 1997-10-08 一郎 中谷 宇宙構造体の相対位置・姿勢検出装置
US5092543A (en) * 1989-09-27 1992-03-03 General Electric Company Spacecraft attitude control with avoidance constraint
JPH0434310A (ja) * 1990-05-31 1992-02-05 Mitsubishi Electric Corp 宇宙機の航法装置
US5347286A (en) * 1992-02-13 1994-09-13 Trimble Navigation Limited Automatic antenna pointing system based on global positioning system (GPS) attitude information
FR2741955B1 (fr) * 1995-12-01 1998-02-06 Matra Marconi Space France Procede et dispositif de mesure d'attitude de satellite
US6072433A (en) * 1996-07-31 2000-06-06 California Institute Of Technology Autonomous formation flying sensor
JP2950279B2 (ja) * 1997-03-26 1999-09-20 日本電気株式会社 目標信号距離測定装置
US6005514A (en) * 1997-09-15 1999-12-21 United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method for attitude determination using GPS carrier phase measurements from nonaligned antennas
US5999127A (en) * 1998-10-06 1999-12-07 The Aerospace Corporation Satellite communications facilitated by synchronized nodal regressions of low earth orbits
US6150977A (en) * 1998-10-30 2000-11-21 Trw Inc. Method for enhancing the performance of a satellite communications system using multibeam antennas
US6459411B2 (en) * 1998-12-30 2002-10-01 L-3 Communications Corporation Close/intra-formation positioning collision avoidance system and method
DE19950247A1 (de) * 1999-10-18 2001-05-17 Daimler Chrysler Ag Regelungsanordnung und Regelungsverfahren für Sstelliten
US6442385B1 (en) * 1999-11-04 2002-08-27 Xm Satellite Radio, Inc. Method and apparatus for selectively operating satellites in tundra orbits to reduce receiver buffering requirements for time diversity signals
US6463365B1 (en) * 2000-02-01 2002-10-08 Raytheon Company System and method for controlling the attitude of a space craft
US6289268B1 (en) * 2000-03-02 2001-09-11 Hughes Electronics Corp. Attitude determination system and method
US6463366B2 (en) * 2000-03-10 2002-10-08 Schafer Corp Attitude determination and alignment using electro-optical sensors and global navigation satellites
US7124001B2 (en) * 2003-07-11 2006-10-17 The Boeing Company Relative attitude estimator for multi-payload attitude determination

Also Published As

Publication number Publication date
JP5007467B2 (ja) 2012-08-22
CN101375176B (zh) 2011-11-23
US8463467B2 (en) 2013-06-11
ES2340062T3 (es) 2010-05-28
WO2007082929A1 (fr) 2007-07-26
RU2419807C2 (ru) 2011-05-27
RU2008133983A (ru) 2010-02-27
CN101375176A (zh) 2009-02-25
EP1813957A1 (fr) 2007-08-01
EP1813957B1 (fr) 2010-03-10
US20110160939A1 (en) 2011-06-30
ATE460680T1 (de) 2010-03-15
JP2009536314A (ja) 2009-10-08

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